EP1746251B1 - Diaphragme d'ensemble d'aubes statoriques assemblé - Google Patents

Diaphragme d'ensemble d'aubes statoriques assemblé Download PDF

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Publication number
EP1746251B1
EP1746251B1 EP06019263.0A EP06019263A EP1746251B1 EP 1746251 B1 EP1746251 B1 EP 1746251B1 EP 06019263 A EP06019263 A EP 06019263A EP 1746251 B1 EP1746251 B1 EP 1746251B1
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EP
European Patent Office
Prior art keywords
diaphragm
outer ring
nozzle
diaphragm outer
insertion portion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP06019263.0A
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German (de)
English (en)
Other versions
EP1746251A1 (fr
Inventor
Takashi Sasaki
Yuji Nakama
Kenichi Imai
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toshiba Corp
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Toshiba Corp
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Publication date
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Publication of EP1746251A1 publication Critical patent/EP1746251A1/fr
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/61—Assembly methods using limited numbers of standard modules which can be adapted by machining
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles

Definitions

  • the present invention relates to an assembled nozzle diaphragm applied to a steam turbine.
  • an axial flow steam turbine having large capacity, including a plurality of sages, arranged along steam flow direction, each comprising in combination a turbine nozzle (turbine stationary (stator) blade) and a turbine moving or movable (rotor) blade.
  • the axial flow steam turbines will be roughly classified into reaction type and impulse type.
  • the steam turbine of the impulse type causes thermal energy of a steam to perform more expansion work using each turbine nozzle, transforms the steam after the expansion work to a deflected flow using each turbine moving blade, and guides the resultant deflected flow to the next stage.
  • the turbine nozzle that converts most of the thermal energy of the steam to kinetic energy, a large pressure difference occurs between a steam inlet and a steam outlet of the turbine nozzle. To deal with this pressure difference, therefore, the turbine nozzle adopts a diaphragm structure as shown in Fig. 24 .
  • the turbine nozzle of the diaphragm structure shown in Fig. 24 is constituted as follows.
  • a ring body 1 is divided into two portions on a horizontal joint surface 2, both ends of nozzle blades (nozzle plates) 3 arranged in ring columns are supported by a diaphragm outer ring 4 and a diaphragm inner ring 5, and a labyrinth packing mounting groove 6 is provided in an inner periphery of the diaphragm inner ring 5 that faces a turbine shaft (not shown).
  • the turbine nozzle is so-called a weld-type turbine nozzle in which at a time when the nozzle blade 3 is connected to the diaphragm outer ring 4 and the diaphragm inner ring 5, the nozzle blade 3 is fixedly attached thereto by welding portions 8a and 8b through wear plates 7a and 7b, respectively, as shown in Fig. 25 .
  • a counter-flow (double flow) turbine that divides the steam flow to a left flow and a right flow at its inlet as shown in Fig. 30
  • the first and second divided-flow nozzle blades 49 and 50 are fixedly attached to the first and second divided-flow diaphragm outer rings 52 and 53 by welding portions 54a and 54b and bottoms of the first and second divided-flow nozzle blades 49 and 50 are fixed by welding portions 54c and 54d using a shared diaphragm inner ring 51 shared between the first and second divided-flow nozzle blades 49 and 50, respectively.
  • Fig. 29 illustrates one example in which manufacturing cost composition ratios of the weld-type turbine nozzle in the form of a circular graph.
  • a welding cost reaches about 38 percents of a total manufacturing cost.
  • it is difficult to mechanize and automate welding operation 100 percents it is difficult to reduce the welding cost itself, accordingly.
  • An assembled nozzle diaphragm having the features of the preamble of claim 1 is known from EP-A-0 384 166 .
  • JP 2000/337103 , GB-A-1263639 , EP-A-0 945 597 , US-A-5,848,854 , US-A-4,826,395 and US-A-3,326,523 disclose a nozzle blade insertion portion to be inserted into a groove in the diaphragm outer ring, which is "T"-shaped.
  • the insertion portion of the nozzle blade to be inserted into a groove in the diaphragm outer ring is formed of a protruded hook portion on only one side and having a base portion and a stepped block portion.
  • This insertion portion is fitted on a protruded portion on a first component of the diaphragm outer ring. After this fitting a second component of the diaphragm outer ring is fixed to the first component of the diaphragm outer ring. It is an object of the present invention to modify and thereby simplify a turbine nozzle structure and to provide an assembled nozzle diaphragm which can be easily assembled without performing a welding operation and a method of assembling such nozzle diaphragm.
  • An assembled nozzle diaphragm according to the present invention comprises the features of claim 1.
  • Fig. 31 illustrates stages of an axial flow steam turbine 100 that provided with the assembled nozzle diaphragm.
  • Each nozzle blade 104 is attached to a diaphragm outer ring 102 attached to a turbine casing 101 and a diaphragm inner ring 103 so as to form a nozzle blade flow path.
  • a plurality of turbine moving (rotor) blades 106 is arranged downstream of this nozzle blade flow path.
  • the moving blades 106 are built up or assembled in columns at predetermined intervals on an outer periphery of a rotor wheel 105 in a circumferential direction, and a cover 107 that prevents leakage of a working fluid is attached to an outer peripheral end of each moving blade 106.
  • the fluid that is, steam ST flows from a right direction (upstream side) of the steam turbine to a left direction (downstream side) thereof.
  • the constituent elements of the assembled nozzle diaphragm are provided at positions shown in Fig. 31 even without so specified.
  • Fig. 1 is an elevational section which illustrates the first embodiment of the assembled nozzle diaphragm not implementings the present invention.
  • the assembled nozzle diaphragm in this embodiment is constituted so that a nozzle blade (nozzle plate) 14 that includes a diaphragm outer ring insertion portion 12 and a diaphragm inner ring insertion portion 13 on both ends, respectively, a diaphragm outer ring 15 to which the diaphragm outer ring insertion portion 12 is fitted and which supports a head of the nozzle blade (nozzle plate) 14, and a diaphragm inner ring 16 to which the diaphragm inner ring insertion portion 13 is fitted and which supports a bottom of the nozzle blade (nozzle plate) 14.
  • the diaphragm outer ring insertion portion 12 is formed together with the nozzle blade 14 by precision casting or by being integrally cut out from a nozzle blade element assembly through a machining process.
  • An upstream side surface portion 19 of the nozzle outer ring insertion portion 12 directed toward a flow of the steam ST in a case where this assembled nozzle diaphragm is incorporated to the steam turbine is formed to be protruded as a whole.
  • This upstream side surface portion 19 is formed as a ring block body including a hook portion 17 and a block portion 18 formed in a step form, and the upstream side surface portion 19 extends in the circumferential direction (a moving blade rotating direction on a perpendicular plane relative to the steam flow).
  • the diaphragm inner ring insertion portion 13 similarly to the diaphragm outer ring insertion portion 12 shown in Figs. 2 and 3 , is formed together with the nozzle blade 14 by precision forging or by being integrally cut out from the nozzle blade element assembly by the machining work.
  • the diaphragm inner ring insertion portion 13 includes a convex columnar piece 20 in an intermediate portion and this columnar piece 20 is formed into a ring block body extending in the circumferential direction.
  • the diaphragm outer ring 15, to which the diaphragm outer ring insertion portion 12 is fitted, is formed as a ring body and divided in half to an outer ring upper half portion 21 and an outer ring lower half portion 22 on a horizontal joint surface HJS 1.
  • the diaphragm outer ring 15 divided in half includes a protruded hook portion 24 at an inlet of a cap or cap-shaped groove 23, and this hook portion 24 applies a pressing force to the stepped block portion 18 of the diaphragm outer ring insertion portion 12 and engages with and supports the hook portion 17 of the diaphragm outer ring insertion portion 12.
  • the presence of the cap-shaped groove 23 and the hook portion 24 of the diaphragm outer ring 15 enables the diaphragm outer ring insertion portion 12 of the nozzle blade 14 to be fitted and inserted into the diaphragm outer ring 15 only on the horizontal joint surface HJS 1 while the nozzle blade 14 cannot be inserted into the diaphragm outer ring 15 in the other regions.
  • the diaphragm outer ring insertion portion 12 When the diaphragm outer ring insertion portion 12 is successively fitted to the cap-shaped groove 23 formed in the diaphragm outer ring 15 and the diaphragm outer ring insertion portion 12 is arranged on an entire periphery of the diaphragm outer ring 15, the outer ring upper half portion 21 and the outer ring lower half portion 22 of the diaphragm outer ring 15 are then fastened by means of bolts 25a and 25b as shown in Fig. 4 .
  • the diaphragm outer ring 15 is engaged with and supported by a casing (not shown).
  • the diaphragm inner ring 16 to which the diaphragm inner ring insertion portion 13 is fitted, is formed as a ring body and divided in half to an inner ring upper half portion 26 and an inner ring lower half portion 27 on a horizontal joint surface HJS2 similarly to the diaphragm outer ring 15.
  • the diaphragm inner ring 16 divided in half includes a concave groove 28 on a head side (outer diameter side) and a labyrinth packing groove 29 on a bottom side (inner diameter side).
  • the diaphragm inner ring insertion portion 13 is fitted to the concave groove 28 on the head side, a labyrinth packing 30 is fitted into the labyrinth packing groove 29, and then the inner ring upper half portion 26 and the inner ring lower half portion 27 are joined together by a key (not shown) as shown in Fig. 6 .
  • the assembled nozzle diaphragm has a structure in which the diaphragm inner ring insertion portion 13 of the nozzle blade 14 is fitted to the diaphragm inner ring 16 through the engagement of the simple concave groove 28 and the simple convex columnar piece 20. Therefore, it is unnecessary to move the diaphragm inner ring 16 from the horizontal joint surface HJS2 in the circumferential direction so as to successively insert the diaphragm inner ring insertion portion 13 of the nozzle blade 14 into the diaphragm inner ring 16, and the diaphragm inner ring insertion portion 13 can be simply inserted thereinto from an inside diameter direction (from a downward direction to an upward direction in Fig. 7 ).
  • stopper pieces 31a and 31b are mounted to the diaphragm outer ring 15 and the diaphragm outer ring insertion portion 12 and also to the diaphragm inner ring 16 and the diaphragm inner ring insertion portion 16 on the horizontal joint surfaces HJS 1 and HJS2, respectively, shown in Fig.
  • the fitting of the diaphragm outer ring insertion portion 12 into the diaphragm outer ring 15 and that of the diaphragm inner ring insertion portion 13 into the diaphragm inner ring 16 arc made for each nozzle blade 14.
  • a nozzle diaphragm block body 33 that binds together a plurality of nozzle blades 14 such as three nozzle blades and allows the nozzle blades 14 to be supported by the diaphragm outer ring 15 and the diaphragm inner ring 16.
  • the fitting dimension of the diaphragm outer ring insertion portion 12 fitted to the diaphragm outer ring 15 is set to be in a range in which a gap of 0.03 to 0.12 millimeters is formed along a surface of the head side of the diaphragm outer ring insertion portion 12 in the flow direction of the steam ST, and a gap of 0.03 to 0.12 millimeters is formed in a surface of the stepped block portion 18 on a diameter direction side (a side orthogonal to the flow direction of the steam ST) as shown in Fig. 1 .
  • the fitting dimension of the diaphragm inner ring insertion portion 13 fitted to the diaphragm inner ring 16 it is most preferable to set the fitting dimension of the diaphragm inner ring insertion portion 13 fitted to the diaphragm inner ring 16 to be in a range in which a gap of 0.03 to 0.12 millimeter is formed on the diameter direction side (side orthogonal to the flow direction of the steam ST) of the columnar piece 20 of the diaphragm inner ring insertion portion 13 as shown in Fig. 1 .
  • each of the fitting dimensions of the diaphragm outer ring insertion portion 12 fitted to the diaphragm outer ring 15 and that of the diaphragm inner ring insertion portion 13 fitted to the diaphragm inner ring 16 to be in the range of 0.03 to 0.12 millimeters is based on the fact that if they are set to be 0.03 millimeters or less, the diaphragm outer and inner ring insertion portions 12 and 13 cannot be assembled manually with the diaphragm outer and inner rings 15 and 16 and that if they exceed 0.12 millimeters, plays are generated and a shakiness occurs to the assembled nozzle diaphragm during the operation.
  • An FEM (finite element method) analysis, a mock-up test or the like also has confirmed that these fitting dimensions are the most appropriate dimensions.
  • the diaphragm outer ring insertion portion 12 is provided on one end of the nozzle blade (nozzle plate) 14, the diaphragm inner ring insertion portion 13 is provided on the other end thereof, the groove 23, to which the diaphragm outer ring insertion portion 12 is fitted, is provided in the diaphragm outer ring 15, and the groove 28, to which the diaphragm inner ring insertion portion 13 is fitted, is provided in the diaphragm inner ring 16, whereby there can be provided the simple assembled structure that does not require welding operation for welding the diaphragm outer ring insertion portion 12 and the diaphragm inner ring insertion portion 13 to the respective grooves 23 and 28. Therefore, during the assembly of the turbine nozzle, a steam path 34 can be kept to have designed dimensions and the turbine nozzle can be operated with an improved turbine stage efficiency at low cost that does not accompany the welding cost.
  • Fig. 21 is a schematic block diagram showing the steps of the method of assembling the nozzle diaphragm.
  • the diaphragm outer ring 15 and the diaphragm inner ring 16, which are ring bodies when the nozzle diaphragm is completed, are manufactured independently as the diaphragm outer ring upper half portion 21 and the diaphragm outer ring lower half portion 22 obtained by dividing the diaphragm outer ring 15 in half at a position of substantially 180 degrees and as the diaphragm inner ring upper half portion 26 and the diaphragm inner ring lower half portion 27 obtained by dividing the diaphragm inner ring 16 in half at a position of substantially 180 degrees, respectively.
  • the grooves into which the nozzle blade 14 is fitted are preliminarily worked in the upper half portions 21 and 26 and the lower half portions 22 and 27.
  • the cap-shaped groove 23 and the hook portion 24 are worked in the diaphragm outer ring upper half portion 21 and the diaphragm outer ring lower half portion 22, respectively, whereas the concave groove 28 is worked in the diaphragm inner ring upper half portion 26 and the diaphragm inner ring lower half portion 27.
  • Shapes of these grooves are set in advance so that the diaphragm outer ring insertion portion 12 and the nozzle blade 14 are surely engaged with the respective grooves.
  • the nozzle blades 14 are sequentially inserted into the worked cap-shaped groove 23 and hook portion 24 from one side of the horizontal joint surface HSJ1.
  • the number of nozzle blades 14 to be inserted is determined in advance based on a pitch circle diameter (PCD) of this diaphragm and a pitch between the nozzle blades 14.
  • PCD pitch circle diameter
  • the first and last inserted nozzle blades 14, i.e., the two nozzle blades 14 facing the horizontal joint surface HSJ1 of the diaphragm outer ring 15 are fixed relative to the circumferential direction so that the nozzle blades 14 do not slip off from the grooves of the outer rings by means of the stopper pieces 31a fixed to the diaphragm outer rings 15.
  • the inserted nozzle blades 14 are fixed relative to the steam flow direction and a nozzle blade longitudinal direction by engaging the hook portions 17 of the diaphragm outer ring insertion portions 12 provided on these nozzle blades 14 with the cap-shaped grooves 23 of the diaphragm outer rings 15 and also engaging the block portions 18 of the diaphragm outer ring insertion portions 12 provided on the nozzle blades 14 with the hook portions 24 of the diaphragm outer rings 15, respectively.
  • mechanical means such as bolts or pins or fixing means such as welding for fitting the diaphragm outer ring insertion portions 12 of the nozzle blades 14 into the respective diaphragm outer rings 15.
  • the diaphragm inner ring 16 is fitted into the diaphragm outer ring 15, to which each nozzle blade 14 is inserted, from the diaphragm inner ring insertion portion side of the nozzle blade 14.
  • the fitting portion has a simple shape consisting of the concave groove 28 provided in the diaphragm inner ring 16 and the convex columnar piece 20 provided on the diaphragm inner ring insertion portion 13 of the nozzle blade 14.
  • each of the diaphragm inner ring 16 is fixed to the nozzle blade 14 by the stopper piece 31 b in a manner such that the stopper piece 31 b fixes the nozzle blade 14 relative to the circumferential direction and fixes the diaphragm inner ring insertion portion 13 of the nozzle blade 14 to the diaphragm inner ring 16 to thereby prevents the diaphragm inner ring 16 from slipping off.
  • the diaphragm upper half portion (or diaphragm lower half portion), in which the diaphragm outer ring 15, the nozzle blade 14 and the diaphragm inner ring 16 are formed integrally, and the diaphragm lower half portion (or diaphragm upper half portion) formed similarly are mated to each other on their horizontal joint surfaces, and then, the nozzle diaphragm is completed by screw-engaging a bolt with a bolt hole provided in the diaphragm outer ring 15 of one of the diaphragm upper and lower half portions and a thread portion provided in the other one of the diaphragm upper and lower half portion.
  • the nozzle blade 14 is not fixed to the diaphragm inner ring 16 and the diaphragm outer ring 15, even if any defect occurs to the nozzle blade during the operation, only the nozzle blade to which the defect occurs can be exchanged without exchanging the entire diaphragm as in the conventional art.
  • the fitting gap between the nozzle blade 14 and the diaphragm inner ring 16 and that between the nozzle blade 14 and the diaphragm outer ring 15 are set to be in the range of 0.03 to 0.12 millimeters, no problem occurs to the nozzle blade insertion operation and the nozzle diaphragm can be operated without shakiness and with no mechanical fixing means even if a vibration is generated by the steam during the turbine operation.
  • Fig. 11 is an elevational section representing the second embodiment of the assembled nozzle diaphragm not implementing the present invention.
  • like reference numerals are added to constituent elements corresponding to those in the first embodiment.
  • a T-shaped groove 35 is formed in the diaphragm outer ring 15, and the diaphragm outer ring insertion portion 12 fitted into this groove 35 is provided with protruded hook portions 38a and 38b formed on an upstream side surface 36 directed toward the flow of the steam ST and on a downstream side 37 directed toward the flow of the steam ST, respectively, stepped block portions 39a and 39b continuous to the respective hook portions, and base portions 40 continuous to the respective block portions.
  • the T-shaped cap groove 35 is formed in the diaphragm outer ring 15, the upstream side surface 36 and the downstream side surface 37 of the diaphragm outer ring insertion portion 12 are also formed by the continuous hook portions 38a and 38b, the block portions 39a and 39b and the base portions 40, respectively, and the hook portions 38a and 38b and the block portions 39a and 39b of the diaphragm outer ring insertion portion 12 are fitted into the groove 35 of the diaphragm outer ring 15, thus providing the simple assembled structure that does not require welding operation. Therefore, during the assembling of the turbine nozzle, a steam path 43 can be kept to have designed dimensions and the turbine nozzle can be operated with highly improved turbine stage efficiency at low cost that does not accompany the welding cost.
  • the so-called I-shaped diaphragm outer ring insertion portion 12 having the protruded hook portions 38a and 38b, the stepped block portions 39a and 39b, and the protruded base portions 40 formed on the upstream side surface 36 and the downstream side surface 37, respectively, is fitted into the T-shaped cap groove 35 formed in the diaphragm outer ring 15 .
  • the diaphragm outer ring insertion portion 12 formed by a columnar piece 42 and a protruded base portion 40 directed toward a diameter direction (a direction orthogonal to the flow of the steam ST) may be formed in a concave groove 41 formed in the diaphragm outer ring 15 and directed toward the diameter direction.
  • the assembling steps of the nozzle diaphragm assembling method in the second embodiment are substantially the same as those in the first embodiment, so that the steps will not be described herein.
  • Fig. 13 is an elevational section representing the fourth embodiment of the assembled nozzle diaphragm not implementing the present invention.
  • Fig. 13 the same constituent elements as those in the second embodiment are denoted by the same reference numerals.
  • a cap or cap-shaped groove 35 provided with a protruded hook portion 24 on an inlet side is formed in the diaphragm outer ring 15.
  • the upstream side surface 36 of the diaphragm outer ring insertion portion 13 which is directed toward the flow of the steam ST is also formed in combination of the protruded hook portion 38a, the stepped block portion 39a and the protruded base portion 40, and a ring piece 44 to be divided is attached to the block portion 39a.
  • a bolt 45 is also provided on the diaphragm outer ring 15 to apply a pressing force to the diaphragm outer ring insertion portion 12, and a coupled surface on which the diaphragm outer ring insertion portion 12m to be fitted to the groove 35, is coupled to the diaphragm outer ring 15 is sealed.
  • the other structures are substantially the same as those of the first embodiment, so that the details thereof are now omitted herein.
  • the continuous hook portion 38a, block portion 39a, and base portion 40 are all formed together with the nozzle blade 14 by precision forging or by being integrally cut out from a nozzle blade element assembly by the machining work.
  • the ring piece 44 is then interposed between the diaphragm outer ring insertion portion 12 and the diaphragm outer ring 15, and the coupled surface 46 between the diaphragm outer ring insertion portion 12 and the diaphragm outer ring 15 is sealed due to the pressing force of the bolt 45 engaged with the diaphragm outer ring 15. Therefore, the shakiness of the turbine nozzle can be surely prevented from causing and the turbine nozzle can be hence operated stably.
  • the coupled surface between the diaphragm outer ring insertion portion 12 and the diaphragm outer ring 15 is sealed. Therefore, it is not necessary to improve or maintain the accuracy of the fitting gap between the diaphragm outer ring insertion portion 12 and the diaphragm outer ring 15, thus reducing the working cost.
  • This nozzle diaphragm assembling method differs from that of the first embodiment in that at a time when the nozzle blade is inserted into the diaphragm outer ring, not only the nozzle blade but also shakiness prevention pieces can be inserted into the diaphragm outer ring and in that the shakiness prevention pieces are fastened by the bolt applied to the hook portion of the diaphragm outer ring to thereby fix or fasten the nozzle blades.
  • the steps other than the above steps are substantially the same as those in the first embodiment shown in Fig. 21 , so that they will not be described herein.
  • Fig. 14 is an elevational section illustrating the assembled nozzle diaphragm according to the fifth embodiment not implementing the present invention.
  • the same constituent elements as those in the second embodiment are denoted by the same reference numerals.
  • the cap groove 35 provided with the protruded hook portion is formed in the inlet-side diaphragm outer ring 15, the upstream side surface 36 of the diaphragm outer ring insertion portion 12 fitted into this groove 35, the surface 36 being directed toward the flow of the steam ST, is formed in combination of the protruded hook portion 38a, the stepped block portion 39a.
  • a shakiness prevention piece 47a is provided on a coupled surface 46a coupled with the diaphragm outer ring 15 on the head side of the protruded hook portion 38a to be parallel to the flow of the steam ST, and a shakiness prevention piece 47b is also provided on a coupled surface 46b on the diameter direction side of the hook portion 38a of the upstream side surface of the diaphragm outer ring insertion portion 12.
  • the shakiness prevention piece 47a prevents the shakiness of the diaphragm outer ring insertion portion 12 in the flow direction of the steam ST (direction of the steam turbine shaft), and on the other hand, the shakiness prevention piece 47b prevents the shakiness of the diaphragm outer ring insertion portion 12 in the diameter direction (direction orthogonal to the flow of the steam ST).
  • the continuous hook portion 38a, block portion 39a, and base portion 40 are all formed together with the nozzle blade 14 by precision forging or by being integrally cut out from a nozzle blade element assembly by the machining work.
  • the coupled surface 46a coupled with the diaphragm outer ring 15 on the head side of the protruded hook portion 38a of the diaphragm outer ring insertion portion 12 parallel to the flow of the steam ST and the coupled surface 46b coupled with the diaphragm outer ring 15 on the diameter direction side of the hook portion 38a are provided with the shakiness prevention pieces 47a and 47b, respectively. Therefore, it is ensured that the shakiness of the turbine nozzle can be prevented from causing and the turbine nozzle can be operated stably.
  • the coupled surfaces 46a and 46b are provided with the shakiness prevention pieces 47a and 47b, respectively, it is not necessary to improve the accuracy of the fitting gap between the diaphragm outer ring insertion portion 12 and the diaphragm outer ring 15, thus reducing the working cost.
  • the coupled surface 46a coupled with the diaphragm outer ring 15 on the head side of the protruded hook portion 38a parallel to the flow of the steam ST and the coupled surface 46b coupled with the diaphragm outer ring 15 on the diameter direction side of the hook portion 38a are provided with the shakiness prevention pieces 47a and 47b, respectively.
  • a shakiness prevention piece 47c may be further provided on a corner (shoulder) portion of the upstream side surface 36 on the head side of the protruded hook portion 38a.
  • the shakiness prevention piece 47c is provided on the corner of the protruded hook portion 38a, it is possible to effectively prevent the shakiness of the diaphragm outer ring insertion portion 12 in both the flow direction of the steam ST and the direction orthogonal to the flow of the steam ST.
  • Fig. 16 is an elevational section illustrating the (seventh) embodiment of the assembled nozzle diaphragm according to the present invention.
  • the same constituent elements as those in the second embodiment are denoted by the same reference numerals.
  • the diaphragm outer ring insertion 12 provided on one end of the nozzle blade (nozzle plate) 14 and the diaphragm outer ring 15, to which this diaphragm outer ring insertion portion 12 is fitted, are constituted substantially equally to those in the fourth embodiment shown in Fig. 14 .
  • a nozzle blade inner periphery-side member 48 is provided, integrally with the nozzle blade 14, on the other end of the nozzle blade 14. That is, in this embodiment, the nozzle blade inner periphery-side member 48 is formed integrally with the nozzle blade 14 in place of the diaphragm inner ring insertion portion 13 and the diaphragm inner ring shown in Fig. 14 .
  • This embodiment is effective for the case in which the distance between the nozzle blade 14 and the turbine shaft, not shown, is small.
  • the nozzle diaphragm assembling method of this fifth to seventh embodiments differs from that in the first embodiment in that when the nozzle blade is inserted into the diaphragm outer ring, not only the nozzle blade but also the shakiness prevention pieces are inserted into the diaphragm outer ring. Further, the other steps are substantially the same as those of the first embodiment shown in Fig. 21 , so that they will not be described herein.
  • Fig. 17 is an elevational section illustrating the eighth embodiment of the assembled nozzle diaphragm not implementing the present invention.
  • the same constituent elements as those in the first embodiment are denoted by the same reference numerals.
  • the assembled nozzle diaphragm in this embodiment is applied to the steam turbine which operates to divide the flow of the steam to the left flow and the right flow, such steam turbine being so-called a counter-flow (double flow) type.
  • First and second divided-flow diaphragm inner ring insertion portions 55 and 57 formed to bottoms of the first and second divided-flow nozzle blades 49 and 50 for the steam ST are provided with convex columnar pieces 57 and 58, respectively.
  • the columnar pieces 57 and 58 are fitted to a shared diaphragm inner ring 51 shared between the first and second divided-flow nozzle blades 49 and 50.
  • the first and second divided-flow diaphragm outer rings 52 and 53 fitted into first and second divided-flow diaphragm outer ring insertion portions 55 and 56 of the first and second divided-flow nozzle blades 49 and 50 are the same in configuration as the outer ring in the first embodiment, so that they will not be described herein.
  • the first and second divided-flow diaphragm inner ring insertion portions 55 and 56 of the first and second divided-flow nozzle blade 49 and 50 are fitted into the shared diaphragm inner ring 51 shared between the first and second divided-flow nozzle blades 49 and 50. It is, therefore, possible to further reduce the manufacturing cost and labor of the worker.
  • the assembled nozzle diaphragm is applied to the steam turbine, it is possible to continuously perform the stable operation for a long term without causing any problem of the distortion based on the welding such as in the conventional art.
  • the assembled nozzle diaphragm of a fitting structure may be applied to so-called tie-in turbine stages constituted so that a first stage diaphragm outer ring 62, to which a first stage nozzle blade 59 and a second stage nozzle blade 60 are fixed through welding portions 61a, 61b, 61c, and 61d, is connected to a second stage nozzle diaphragm outer ring 64 by means of bolt 66.
  • the assembled nozzle diaphragm may be applied only to the first stage nozzle diaphragm outer ring 62 and the second stage nozzle diaphragm outer ring 64 or up to a first stage nozzle diaphragm inner ring 63 and a second stage nozzle diaphragm inner ring 65.
  • Fig. 18 is an elevational section illustrating the ninth embodiment of the assembled nozzle diaphragm not implementing the present invention.
  • Fig. 18 the same constituent elements as those in the first embodiment are denoted by the same reference numerals.
  • multiple-stage diaphragm outer ring insertion portions 69 such as a first stage nozzle diaphragm outer ring insertion portion 67 of a first stage nozzle blade 59 and a second stage diaphragm outer ring insertion portion 68 of a second stage nozzle blade 60 are collectively fitted into a multiple-stage diaphragm outer ring 70.
  • the multiple-stage diaphragm outer ring insertion portions 69 such as the first stage nozzle diaphragm outer ring insertion portion 67 of the first stage nozzle blade 59 and the second stage diaphragm outer ring insertion portion 68 of the second stage nozzle blade 60 are collectively fitted to the multiple-stage diaphragm outer ring 70. Therefore, when the assembling operation is performed, the number of assembling steps and labor of the workers can be further reduced.
  • Fig. 19 is an elevational section illustrating the tenth embodiment of the assembled nozzle diaphragm not implementing the present invention.
  • the same constituent elements as those in the first embodiment are denoted by the same reference numerals.
  • a plate 71 of a fixed type is inserted into the diaphragm inner ring 16 in the circumferential direction.
  • the other constituent elements are substantially the same as those in the first embodiment, so that they will not be described herein.
  • the stiffness of the assembled nozzle diaphragm can be intensified by inserting the fixed plate 71 into the diaphragm inner ring 16. It is therefore possible to effectively deal with cracks and the like based on an unexpected vibration resulting from an intermittent fluctuation in the steam flow or a pressure fluctuation.
  • This embodiment will be particularly effective for the case that the diaphragm inner ring has low stiffness.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Claims (5)

  1. Membrane de buse assemblée, comprenant :
    un volant extérieur de membrane (15) divisé en moitiés, une rainure en forme de chapeau (35) usinée dans le volant extérieur de membrane, la rainure en forme de chapeau (35) comportant une partie crochet saillante (24), la rainure (35) étant ouverte vers un côté diamètre intérieur et continue dans une direction périphérique intérieure du volant extérieur de membrane (15) ; et
    une pluralité de volets de buse (14) possédant chacun une partie d'insertion (12), les parties d'insertion (12) étant insérées dans la rainure du volant extérieur de membrane (15) et prévues sur une extrémité des volets de buse (14),
    caractérisée en ce que seulement la surface côté amont (36) de la partie d'insertion (12), qui est dirigée vers l'écoulement fluidique, est pourvue d'une partie crochet saillante (38a) et comporte une partie base (40) et une partie bloc épaulée (39a) et,
    en ce qu'un volant intérieur de membrane est constitué d'éléments côté périphérie intérieure (48) formés intégralement avec les volets de buse (14) sur l'autre extrémité de celui-ci ; et
    en ce que le volant extérieur de membrane (15) est divisé en moitiés en une partie moitié supérieure de volant extérieur de membrane (21) et une partie moitié inférieure de volant extérieur de membrane (22) sur une surface de joint horizontal (HJS1).
  2. Membrane de buse assemblée selon la revendication 1, dans laquelle le volant extérieur de membrane (15) comprend une pièce de prévention d'instabilité (47a, 47b) sur une surface d'ajustement sur laquelle la partie d'insertion (12) du volant extérieur de membrane prévue sur le volet de buse (14) correspondant est ajustée sur le volant extérieur de membrane.
  3. Membrane de buse assemblée selon la revendication 1 ou 2, comprenant une première pièce de prévention d'instabilité sur le côté tête de la partie crochet saillante (38a) et une seconde pièce de prévention d'instabilité (47b) prévue sur le côté direction de diamètre de la partie crochet saillante (38a).
  4. Membrane de buse assemblée selon la revendication 1 ou 2, dans laquelle la pièce de prévention d'instabilité est prévue sur une partie de coin sur le côté tête de la partie crochet saillante (38a).
  5. Membrane de buse assemblée selon la revendication 1, dans laquelle une pièce de volant divisée (44) est fixée aux parties bloc étagées (39a) et un boulon (45) est prévu sur le volant extérieur de membrane (15) afin d'appliquer une force de pression sur la partie d'insertion (12) du volant extérieur de membrane.
EP06019263.0A 2001-07-19 2002-07-18 Diaphragme d'ensemble d'aubes statoriques assemblé Expired - Lifetime EP1746251B1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2001219997 2001-07-19
JP2002207392A JP4040922B2 (ja) 2001-07-19 2002-07-16 組立式ノズルダイアフラムおよびその組立方法
EP02747692.8A EP1408198B1 (fr) 2001-07-19 2002-07-18 Membrane de buse de type a assembler et procede d'assemblage

Related Parent Applications (2)

Application Number Title Priority Date Filing Date
EP02747692.8 Division 2002-07-18
EP02747692.8A Division EP1408198B1 (fr) 2001-07-19 2002-07-18 Membrane de buse de type a assembler et procede d'assemblage

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EP1746251A1 EP1746251A1 (fr) 2007-01-24
EP1746251B1 true EP1746251B1 (fr) 2013-11-13

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EP02747692.8A Expired - Lifetime EP1408198B1 (fr) 2001-07-19 2002-07-18 Membrane de buse de type a assembler et procede d'assemblage
EP06019263.0A Expired - Lifetime EP1746251B1 (fr) 2001-07-19 2002-07-18 Diaphragme d'ensemble d'aubes statoriques assemblé

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EP (2) EP1408198B1 (fr)
JP (1) JP4040922B2 (fr)
KR (2) KR100628907B1 (fr)
CN (2) CN100473804C (fr)
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WO2003008765A1 (fr) 2003-01-30
KR100628907B1 (ko) 2006-09-27
CN1533466A (zh) 2004-09-29
EP1408198A4 (fr) 2005-01-05
EP1408198B1 (fr) 2013-07-03
KR20040018477A (ko) 2004-03-03
US20040253095A1 (en) 2004-12-16
CN101403320B (zh) 2012-09-19
JP4040922B2 (ja) 2008-01-30
EP1746251A1 (fr) 2007-01-24
AU2002318750B2 (en) 2007-05-24
AU2007200325A1 (en) 2007-02-15
CN101403320A (zh) 2009-04-08
EP1408198A1 (fr) 2004-04-14
CN100473804C (zh) 2009-04-01
KR20060060056A (ko) 2006-06-02
US7179052B2 (en) 2007-02-20
JP2003097218A (ja) 2003-04-03
AU2007200325B2 (en) 2009-03-26

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